Abstract We consider a turbofan engine (TFE), where the turbine rotor blades of the low pressure turbine (LPT) are micro-Laval nozzles. We demonstrated the possibility of integrating the super jet turbine and a jet nozzle as a single binary system for the purpose of generation of powerful coherence radiation. We estimated the efficiency of the binary high pressure emitting system being a TFE part.


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    Titel :

    Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 60 , 3 ; 474-477


    Erscheinungsdatum :

    2017-07-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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